A medium-sized jet has a 3.8-m-diameter fuselage and a loaded mass of 85,000 kg. The drag on an airplane is primarily due to the cylindrical fuselage, and aerodynamic shaping gives it a drag coefficient of 0.37. Part A How much thrust must the jet's engines provide to cruise at 240 m/s at an altitude where the air density is 1.9 kg/m³? Express your answer with the appropriate units.

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A medium-sized jet has a 3.8-m-diameter fuselage and a loaded mass of 85,000 kg. The drag on an
airplane is primarily due to the cylindrical fuselage, and aerodynamic shaping gives it a drag
coefficient of 0.37.
Part A
How much thrust must the jet's engines provide to cruise at 240 m/s at an altitude where the air
density is 1.9 kg/m³?
Express your answer with the appropriate units.
Transcribed Image Text:A medium-sized jet has a 3.8-m-diameter fuselage and a loaded mass of 85,000 kg. The drag on an airplane is primarily due to the cylindrical fuselage, and aerodynamic shaping gives it a drag coefficient of 0.37. Part A How much thrust must the jet's engines provide to cruise at 240 m/s at an altitude where the air density is 1.9 kg/m³? Express your answer with the appropriate units.
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